A free stream fluid kinetic energy conversion device combines a large diameter freewheeling primary rotor with small diameter secondary power takeoff rotors placed within the lift induced blade tip vortices of the primary rotor. This enables use of high rotational speed generating units and avoids diseconomy of scale in gearbox expense. The device partially recovers otherwise lost blade tip vortex energy. The freewheeling primary rotor transmits no reaction torque to the support structure. Resilient buoyant tether deployment accommodates transient eddy induced structural loads.
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1. A free stream fluid kinetic energy conversion device deployed in an environment that contains a fluid, comprising:
a primary rotor including two or more lift producing foils that rotate to develop a respective trailing vortex at each distal end of said two or more lift producing foils in response to a flow of the fluid being received by the primary rotor, and
a secondary rotor deployed within each trailing vortex,
wherein:
said secondary rotors are further respectively positioned substantially coaxial to their corresponding said trailing vortex, and
said secondary rotors respectively rotate in the same direction as their corresponding said trailing vortex, and
said secondary rotors drive integral electric generators.
2. The energy conversion device of
a neutrally buoyant resilient tether disposed in the water and having communication with the primary rotor, the neutrally buoyant resilient tether opposing a drag force in said flow of the water,
wherein a lower end of said neutrally buoyant resilient tether is pivotably attached to the floor and an upper end of said neutrally buoyant resilient tether is vertically supported by a cable attached to a water surface buoy.
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This application claims benefit of U.S. Provisional Application Ser. No. 61/622,250 filed Apr. 10, 2012 fully incorporated herein by reference.
Aspects of the present invention are directed to conversion of hydrokinetic and wind energy to electrical energy.
Large scale economic conversion of rotary hydrokinetic power must address the challenge of extremely slow rotation with extremely high torque. Modern wind power conversion shares this challenge, but the higher viscosity of water imposes an even lower functional limit on turbine blade tip speed. Engineering designs to meet this challenge are high in cost, including large gear boxes, direct drive generating units, or hydraulic transmissions. This challenge increases with turbine diameter.
The present invention is a value engineering solution to enable economic deployment of large diameter horizontal axis hydrokinetic turbines. A large freewheeling turbine incorporates secondary turbines at the tips of its blades where localized energy density is greatest. In effect, this arrangement employs the ambient fluid as a planetary gear ring. The required generating units are economical high speed type.
The secondary turbines are positioned in way of the induced primary rotor blade tip vortices to partially recover that rotational energy. In this arrangement, vortex energy recovery provides the further benefit of dissipating vortex drag, which is otherwise a significant drag upon free stream energy conversion rotors.
Because no torque is translated through the primary turbine shaft, there is significant structural savings in avoided reaction torque support.
In the prior art, the Minesto Company has proposed a kite-turbine that also incorporates a secondary turbine. It flies in a dynamically controlled figure-eight path at reported speeds up to ten times the ambient current speed. In comparison, the present invention does not expend energy in tether motion and partially recovers induced wing tip vortex energy that is otherwise a source of drag.
The prior art describes means to recover wing-tip vortex energy in fixed wing aircraft, for example U.S. Pat. No. 4,428,711 to Archer, U.S. Pat. No. 4,917,332 to Patterson, U.S. Pat. No. 5,100,085 to Rubbert, U.S. Pat. No. 5,150,859 to Ransick, U.S. Pat. No. 5702,071 to Kroll et al., U.S. Pat. No. 5,918,835 to Gerhardt, and U.S. Pat. No. 5,934,612 to Gerhardt. For wind energy conversion, the prior art also describes means to convert induced vortex energy from other non-rotating forms, for example U.S. Pat. No 4,045,144 to Loth, U.S. Pat. No 4,105,362 to Sforza, and U.S. Pat. No. 7,131,812 to Brueckner. The present invention is distinguished by the combination of primary and secondary rotors in a single device.
In
In an alternative embodiment, secondary turbines 230 incorporate high pressure positive displacement pumps not shown, which convey power through a known alternate fluid circuit.
Lastly, the exploded view in
Operation
To place into or remove from service, a vessel not shown engages lift cable 60 to lower or lift cavity 70 onto or off of piling 40.
During natural intervals of slow current in direction A, the inherent stiffness of tether 100 prevents entanglement with or adverse disruption of sea floor 20.
During natural intervals of slow current in direction A, negative buoyancy of turbine 200 causes an increase in angle B, which avoids entanglement of turbine 200 with both tether 100 and cable 112.
During natural intervals of changes in current direction A, the inherent stiffness of tether 100 translates drift motion of the device into rotation of link 50 upon piling 40.
When generating power, negative buoyancy of turbine 200 balances current drag force on turbine 200 to maintain angle B. When at angle B, dihedral angle C causes foils 220 to be more normal to direction A in the lower portion of their rotations, where current velocity is naturally lower, and less normal to direction A in the upper portion of their rotations, where current velocity is naturally higher.
Dihedral angle C further acts to shed jetsam that may entangle the device.
Rotation of turbine 200 in direction D causes increased resultant current velocity at the distal ends of foils 220 where secondary turbines 230 operate. This localized increase in energy density enables economic power conversion. Because secondary turbines 230 operate in rotating fluid, their blade angle of attack is higher than in linear flow, which results in higher torque generation. Also, local pressure drop in the trailing vortex cores acts to draw water 10 through secondary turbines 230. In these ways, rotational direction E vortex energy is partially recovered by co-rotation of secondary turbines 230.
Because power conversion in secondary turbines 230 is integral to their respective foils 220, no torque is translated into shaft 210, which results in manufacturing economy.
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